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Titan I STAGE2 — NASA Sp8089 Injector Designs
98.9 %, 80,000 lbf, 682 psi
Titan I stage2 nasa sp8089 injector designs reference data. This dataset covers 1 row. Key parameters: num elements oxidizer 328 dimensionless; num elements fuel 392 dimensionless; eta c 98.9 %.
- Body Material
- 347 Cres
- Chamber Pressure Psi (psi)
- 682
- Combustion Stabilization
- None
- Element Type
- Like Doublet
- Eta C Pct (%)
- 98.9
- Face Material
- 347 Cres
- Injector Diameter in (in)
- 14.2
- Num Elements Fuel (dimensionless)
- 392
- Num Elements Oxidizer (dimensionless)
- 328
- Orifice Dia Fuel in (in)
- 0.052
- Orifice Dia Oxidizer in (in)
- 0.085
- Propellants
- LOX/RP-1
- Thrust Condition
- Vac
- Thrust Lbf (lbf)
- 80,000
- Vehicle
- Titan I Stage 2